# Service difficulty reports: N306PQ

A list on [N306PQ](https://openairdocs.org/aircraft/N306PQ.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 2 · 52 reports

- [SDR REXA2024102901127](https://openairdocs.org/sdr/REXA2024102901127.md): Floorbeam · cracked · Apr 11, 2024 · N306PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > R/H COCKPIT FLOOR BEAM IS CRACKED IN LOWER O/B FWD RADIUS AT FS 280 REPAIRED RIGHT COCKPIT FLOOR BEAM AT RBL12 IAW MHIRJ REO 690-53-11-1716 REV-- DATED 2024-04-08
- [SDR REXA2024102901126](https://openairdocs.org/sdr/REXA2024102901126.md): Floorbeam · cracked · Apr 11, 2024 · N306PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > L/H COCKPIT FLOOR BEAM IS CRACKED IN LOWER O/B FWD RADIUS AT FS 280 REPAIRED LEFT COCKPIT FLOOR BEAM AT LBL12 IAW MHIRJ REO 690-53-11-1716 REV-- DATED 2024-04-08
- [SDR REXA2024102901125](https://openairdocs.org/sdr/REXA2024102901125.md): Drag Angle · deformed · Mar 31, 2024 · N306PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > AFTER REMOVAL OF PAX DOOR DRAG ANGLE FOUND HOLES ON WEB COMMON TO BE ENLARGE AND FOUND 1EA DOUBLE DRILL HOLE. REPAIRED IAW ENDEAVOR AIR EA CRJ952-16330 REV-A DATED 4/5/2024.
- [SDR REXA2024102801069](https://openairdocs.org/sdr/REXA2024102801069.md): Lug · deformed · Mar 31, 2024 · N306PQ · Cndair CL6002D24 · Ailerons
  > "FOUND BOTH LUGS LABELED ""C"" & ""F"" ON THE R/H AILERON ARE PREVIOUSLY OVERSIZED. FABRICATION OF O/S BUSHINGS (QTY. 2) IS REQUIRED. REPAIRED IAW BOMBARDIER REO 670-57-61-237 REV-- DATE 2017-07-25. "
- [SDR REXA2024061400436](https://openairdocs.org/sdr/REXA2024061400436.md): Drag Angle · cracked · Mar 31, 2024 · N306PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR AFT DRAG ANGLE IS CRACKED. INSTALLED PAX DOOR AFT DRAG ANGLE WITH PN 601R311772-5 IAW CRJ900 SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, 51-42-22-001-001-A01 AND 51-42-15-001-001-A01.
- [SDR REXA2024102801068](https://openairdocs.org/sdr/REXA2024102801068.md): Attach Fitting · corroded · Mar 28, 2024 · N306PQ · Cndair CL6002D24 · Fuselage, Equipment Attach Fittings
  > CORROSION FOUND ON GALLEY ATTACHMENT FITTING BETWEEN FS 280-295 AT RBL 27. GALLEY MOUNTING BRACKET AT RBL 27 F.S. 280 - F.S. 295 IS IDENTIFIED AS P/N SH670-32149-3 AND HAS CORROSION PRESENT BOTH AROUND AND INSIDE OF BOLT HOLE AND IS FOUND TO BE OUT OF
- [SDR REXA2024040900346](https://openairdocs.org/sdr/REXA2024040900346.md): Fitting · corroded · Mar 28, 2024 · N306PQ · Cndair CL6002D24 · Fuselage, Equipment Attach Fittings
  > CORROSION FOUND ON GALLEY ATTACHMENT FITTING BETWEEN FS 280-295 AT RBL 18. GALLEY MOUNTING BRACKET AT RBL 18 F.S. 280 - F.S. 295 IS IDENTIFIED AS P/N SH670-32149-3 AND HAS CORROSION PRESENT BOTH AROUND AND INSIDE OF BOLT HOLE AND IS FOUND TO BE OUT OF L
- [SDR REXA2024040900345](https://openairdocs.org/sdr/REXA2024040900345.md): Crossbeam · corroded · Mar 28, 2024 · N306PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > R/H FS280 CROSSBEAM CORRODED BETWEEN BL0 AND RBL 11. REPAIRED R/H FS280 CROSSBEAM CORRODED BETWEEN BL0 AND RBL 11 IN ACCORDANCE WITH MHIRJ REO 690-53-11-1717 DATE 2024-03-29 REV (--). SEE SHEET 2 FOR DTI REQUIREMENTS
- [SDR REXA2024102901122](https://openairdocs.org/sdr/REXA2024102901122.md): Floorbeam · corroded · Mar 26, 2024 · N306PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > FS 280 FWD J-ANGLE IS CORRODED INSTALLED J-ANGLE PN: CC670-34095-1 AT FS 280 BETWEEN RBL 11 TO LBL 11 IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
- [SDR REXA2024102801066](https://openairdocs.org/sdr/REXA2024102801066.md): Lug · deformed · Mar 26, 2024 · N306PQ · Cndair CL6002D24 · Ailerons
  > "FOUND BOTH LUGS LABELED ""C"" & ""F"" ON THE L/H AILERON ARE PREVIOUSLY OVERSIZED. FABRICATION OF O/S BUSHINGS (QTY. 2) IS REQUIRED. REPAIRED IAW BOMBARDIER REO 670-57-61-237 REV-- DATE 2017-07-25. "
- [SDR REXA2024040900343](https://openairdocs.org/sdr/REXA2024040900343.md): Lug · cracked · Mar 25, 2024 · N306PQ · Cndair CL6002D24 · Emergency Exits
  > RH FWD EMERGENCY EXIT DOOR FORMER CRACKED AT UPPER ALIGNMENT LUG REPAIRED BY COMPLYING WITH ENDEAVOR AIR EA CRJ952-16266 REV IR DATED 4 APR 2024
- [SDR REXA2024040900342](https://openairdocs.org/sdr/REXA2024040900342.md): Lug · cracked · Mar 25, 2024 · N306PQ · Cndair CL6002D24 · Emergency Exits
  > L/H FWD EMERGENCY EXIT DOOR FORMER CRACKED AT UPPER ALIGNMENT LUG. REPAIRED LH FWD EMERGENCY EXIT DOOR UPPER ALIGNMENT LUG BY COMPLYING WITH ENDEAVOR AIR EA CRJ952-16265 REV IR DATED 4 APR 2024
- [SDR REXA2024040900340](https://openairdocs.org/sdr/REXA2024040900340.md): Bracket · cracked · Mar 25, 2024 · N306PQ · Cndair CL6002D24 · Emergency Exits
  > L/H AFT EMERGENCY EXIT DOOR UPPER FWD DOOR ALIGNMENT BRACKET IS CRACKED AT BASE OF BRACKET, REPAIRED LH AFT EMERGENCY EXIT DOOR UPPER FWD DOOR ALIGNMENT BRACKET BY COMPLYING WITH ENDEAVOR AIR EA CRJ952-16264 REV IR DATED 4 APR 2024
- [SDR REXA2024011800089](https://openairdocs.org/sdr/REXA2024011800089.md): Engine · fluctuates · Jan 14, 2024 · N306PQ · Cndair CL6002D24 · Engine (Turbine/Turboprop)
  > WHILE CLIMBING OUT OF ORF THROUGH 13,000' PILOT HEARD A LOUD NOISE. LH ENG N1 WAS FLUCTUATING BETWEEN 30%-60% AND RUNNING ROUGH. FOLLOWED SEVERE ENGINE DAMAGE CHECKLIST AND SHUT DOWN LH ENG. AIRCRAFT CURRENTLY AOS WITH ENGINE CHANGE.
- [SDR REXA2022020100209](https://openairdocs.org/sdr/REXA2022020100209.md): Pseu · none · Jan 29, 2023 · N306PQ · Cndair CL6002D24 · Landing Gear Retraction/Extension System
  > LEVELED OFF AT FL250 AT 290 KTS. HEARD A NOISE IN THE NOSE GEAR BAY ALONG WITH A SLIGHT SHUDDER, FOLLOWED BY A GEAR DISAGREE WARNING. NOISE AND SHUDDER REOCCURRED AS WARNING EXTINGUISHED. INSUFFICIENT TIME BEFORE WARNING EXTINGUISHED TO PERFORM QRH ITEMS. REMO
- [SDR REXA2020122300847](https://openairdocs.org/sdr/REXA2020122300847.md): Hinge · damaged · Dec 11, 2020 · N306PQ · Cndair CL6002D24 · Rudder Structure
  > RUDDER CENTER HINGE BEARINGS 2 EA HAVE EXCESSIVE PLAY. FOUND BOTH CENTER HINGE FITTINGS TO HAVE BORE DAMAGE. REMOVED, DRILLED UP, & INSTALLED 2 EA HINGE FITTINGS P/N: AV67021081-015 & AV67021081- 013, IAW CRJ 900 SRM 51-40-11-001-001-A01 & 51-42-21-001-001-A
- [SDR REXA2020122300844](https://openairdocs.org/sdr/REXA2020122300844.md): Hinge · damaged · Dec 11, 2020 · N306PQ · Cndair CL6002D24 · Rudder Structure
  > RUDDER CENTER HINGE BEARINGS 2 EA HAVE EXCESSIVE PLAY. FOUND BOTH CENTER HINGE FITTINGS TO HAVE BORE DAMAGE. REMOVED, DRILLED UP, & INSTALLED 2 EA HINGE FITTINGS P/N: AV67021081-015 & AV67021081-013, IAW CRJ 900 SRM 51-40-11-001-001-A01 & 51-42-21-001-001-A0
- [SDR REXA2020122300843](https://openairdocs.org/sdr/REXA2020122300843.md): Channel · gouged · Dec 11, 2020 · N306PQ · Cndair CL6002D24 · Vertical Stabilizer
  > VERTICAL STAB LEADING EDGE, PUNCTURE ON CHANNEL 1.5 INCH, MARKED WITH ORANGE TAPE. FABRICATED CHANNEL, IAW CRJ 900 SRM 51-24-21-001-001-A01 REV 38 DATED 72-25-20 AND SRM 51-24-36-001-001-A01 AND 51-40-11-001-001-A01 AND INSTALLED PER SRM 51-42-06-001-001-A01.
- [SDR REXA2020122300850](https://openairdocs.org/sdr/REXA2020122300850.md): Angle · corroded · Dec 10, 2020 · N306PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FS 280 FWD J-ANGLE IS CORRODED. MAINTENANCE PERFORMED CORRECTIVE ACTION NR 1, IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.
- [SDR REXA2020122300841](https://openairdocs.org/sdr/REXA2020122300841.md): Door Sill · corroded · Dec 7, 2020 · N306PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AFT BAGGAGE BAY DOOR CUTOUT LOWER THRESHOLD CORROSION INDICATIONS FS 1020 TO FS 1045, FOUR PLACES AS MARKED. REMOVED & REPLACED AFT CARGO DOOR SILL P/N MM670-35655-003, IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, 51-42-21-001-001-A01, 51-40-11
- [SDR REXA2020122300846](https://openairdocs.org/sdr/REXA2020122300846.md): Door Frame · corroded · Dec 6, 2020 · N306PQ · Cndair CL6002D24 · Fuselage Main, Structure
  > FS 280.00 BULKHEAD, LT DOOR FRAME SKIN IS CORRODED AT FLOOR LEVEL. REPAIRED FS 280.00 BULKHEAD LT DOOR FRAME SKIN, IAW REO 670-53-11-745 REV-A DATED 2016/10/28.
- [SDR REXA2020122300849](https://openairdocs.org/sdr/REXA2020122300849.md): Bracket · corroded · Dec 5, 2020 · N306PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FWD CARGO BAY BRACKET IS CORRODED BETWEEN FS 565 TO FS 580 AT STGR 27. LOCATED AND INSTALLED BRACKET PN SH670-33389-2 AT FS 565-580 STRINGER 27, IAW CRJ 900 SRM 51-42-21-001-001-A01 AND IAW CRJ 900 SRM 51-42-22- 001-001-A01.
- [SDR REXA2020122300848](https://openairdocs.org/sdr/REXA2020122300848.md): Floor Support · corroded · Dec 4, 2020 · N306PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > PAX DOOR SURROUND STRUCTURE HAS CORROSION ON MID FLOOR SUPPORT ANGLE. REMOVED AND REPLACED ANGLE, IAW CRJ 900 SRM 51-42-06-001-A01.
- [SDR REXA2020122300845](https://openairdocs.org/sdr/REXA2020122300845.md): Angle · corroded · Dec 4, 2020 · N306PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > PAX DOOR SURROUND STRUCTURE HAS CORROSION ON SILL ANGLE. REMOVED AND REPLACED PAX DOOR SILL ANGLE, IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
- [SDR REXA2020122300842](https://openairdocs.org/sdr/REXA2020122300842.md): Angle · corroded · Dec 4, 2020 · N306PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ACROSS SERVICE DOOR LOWER SILL. REMOVED & REPLACED SERVICE DOOR LOWER SILL P/N: SH670-31996-3, IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-21-001-001-A01.
- [SDR REXA2019101021395](https://openairdocs.org/sdr/REXA2019101021395.md): Lens · cracked · Oct 2, 2019 · N306PQ · Cndair CL6002D24 · Emergency Lighting
  > PAX DOOR EXTERNAL EMERGENCY LIGHT LENS IS CRACKED. REMOVED AND REPLACED PAX DOOR EMERGENCY LIGHT LENS IAW AMM 33-51-15.
- [SDR REXA2019060740813](https://openairdocs.org/sdr/REXA2019060740813.md): Battery Pack · inoperative · Jun 4, 2019 · N306PQ · Cndair CL6002D24 · Emergency Lighting
  > DURING PRE FLIGHT INSPECTION EMERGENCY EXIT LIGHTING ON THE LOWER SIDE WALL AT ROW 13 FOUND TO BE INOP ON BOTH SIDES. REPLACED BATTERY PACK (EMERGENCYLIGHTS) AT PS 38 IAW CRJ 900 AMM 33-51-17 OPS TEST GOOD THIS CLEARS MEL MM02 UPDATED PLACARD REMOVED MOC NOTI
- [SDR REXA2018082970725](https://openairdocs.org/sdr/REXA2018082970725.md): Oxygen Mask · no test · Aug 27, 2018 · N306PQ · Cndair CL6002D24 · Crew Oxygen System
  > FIRST OFFICER`S OXYGEN MASK WILL NOT SHUT OFF DURING TEST. R & R THE OXYGEN MASK IAW AMM 35-11-12. OPS CHECKED NORMAL.
- [SDR REXA2018082180708](https://openairdocs.org/sdr/REXA2018082180708.md): Flashlight · inoperative · Aug 18, 2018 · N306PQ · Cndair CL6002D24 · Emergency Equipment
  > FA FLASHLIGHT NOT CHARGING, NO CHARGE LIGHT SHOWN. REPLACED THE FLASHLIGH BATTERY IAW AMM
- [SDR REXA2017092901044](https://openairdocs.org/sdr/REXA2017092901044.md): Oxygen Mask · unwanted deploy · Sep 29, 2017 · N306PQ · Cndair CL6002D24 · Passenger Oxygen System
  > OXYGEN MASK ON FA JUMPSEAT DEPLOYED AFTER LANDING. STOWED THE FLT ATTENDANT OXYGEN MASK IAW AMM 35-11-12. OK FOR SERVICE
- [SDR REXA2017092001017](https://openairdocs.org/sdr/REXA2017092001017.md): Seal · broken · Sep 20, 2017 · N306PQ · Cndair CL6002D24 · Emergency Equipment
  > RED SEAL ON PBE IN COCKPIT BROKEN. INSTALLED THE SEAL IAW AMM 35-31-06.
- [SDR REXA2017081200883](https://openairdocs.org/sdr/REXA2017081200883.md): Unknown · odor · Aug 12, 2017 · N306PQ · Cndair CL6002D24 · Air Distribution System
  > ODOR OF AN OVERHEATING MOTOR WITH RECIRCULATION FAN ON, GOES AWAY WITH FAN OFF. PULLED AND COLARD CIRCUIT BREAKER 1 A5, 2 A5. RAN RECIRCULATION FANS FOR TWO HOURS AND PERFORMED OPERERATIONAL TEST IAW AMM 21-22-10. ALL CHECKED GOOD NO ODOR NOTED AT THIS
- [SDR REXA2017050800575](https://openairdocs.org/sdr/REXA2017050800575.md): Fan · inoperative · May 8, 2017 · N306PQ · Cndair CL6002D24 · Air Distribution Fan
  > BOTH FA'S REPORTED HEAVY ELECTRICAL ODOR IN FWD PART OF CABIN BETWEEN ROW1 AND FA JUMPSEAT. OVEN NOT IN USE. NO SMOKE OBSERVED. ACCOMPLISHED + INSPECTED AREA FOR SMELL PER FIM 21-22-00. ISOLATED SMELL COMING FROM LEFT PACK. DEFERRED LEFT PACK PER MEL 21-51-1B.
- [SDR REXA2017040400440](https://openairdocs.org/sdr/REXA2017040400440.md): Stringer · corroded · Apr 4, 2017 · N306PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STR 27 HAS CORROSION SPOTS BETWEEN FRAMES 319.70 TO JUST FWD OF FRAME 310, IN THE FWD E & E BAY. OUT OF LIMITS. REPAIRED STR 27 IAW EA CRJ953-05486 REV IR.
- [SDR REXA2017040100430](https://openairdocs.org/sdr/REXA2017040100430.md): Channel · cracked · Apr 1, 2017 · N306PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > DIAPHRAM JUST TO THE RIGHT OF STGR 27 HAS CORROSION BETWEEN FRAMES 364 AND 349, IN THE FWD E&E BAY. REMOVED AND REPLACED DIAPHRAM RIGHT OF STGR 27, FR 364-FR 349 IAW SRM 51-42-06 + 51-42-21 OPS TEST OF THE MAIN AVIONICS DOOR IS GOOD IAW AMM 52-42-00-710-801.
- [SDR REXA2017040100439](https://openairdocs.org/sdr/REXA2017040100439.md): Handle · cracked · Apr 1, 2017 · N306PQ · Cndair CL6002D24 · Electrical/Electronic Compartment Doors
  > MAIN AVINICS COMPT. DOOR OUTER HANDLE IS CRACKED. REMOVED AND REPLACED AVIONICS DOOR HANDLE IAW AMM 52-42-02. OPS TEST OF THE MAIN AVIONICS DOOR GOOD IAW AMM 52-42-00-710-801.
- [SDR REXA2017033100432](https://openairdocs.org/sdr/REXA2017033100432.md): Drag Angle · cracked · Mar 31, 2017 · N306PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > MAIN ENTRY DOOR AFT DRAG ANGLE IS CRACKED. REPAIRED ENTRY DOOR AFT DRAG BRACE ANGLE IAW REO 670-52-11-072.
- [SDR REXA2017033100433](https://openairdocs.org/sdr/REXA2017033100433.md): Channel · corroded · Mar 31, 2017 · N306PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > (OK TO INSTALL TCAS CHANNEL) STGR27 CORRODED AT FS295. REMOVED AND REPLACED STRINGER AND RESTORED FINISH IAW SRM 51-42-06, 51-42-21 AND 51-25-16.
- [SDR REXA2017033000431](https://openairdocs.org/sdr/REXA2017033000431.md): Channel · cracked · Mar 30, 2017 · N306PQ · Cndair CL6002D24 · Aerodynamic Fairings
  > AFT WING TO BODY FAIRING SPLICE CHANNEL IS CRACKED. REMOVED CRACKED CHANNEL ON AFT WING TO BODY FAIRING, AND REPLACED W/NEW SERV CHANNEL IAW SRM 51-42-13.
- [SDR REXA2017032900436](https://openairdocs.org/sdr/REXA2017032900436.md): Crossbeam · corroded · Mar 29, 2017 · N306PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > RT 280 CROSSBEAM IS CORRODED. REMOVED AND REPLACED WITH NEW BEAM PER SRM 51-42-06, 51-42-13 AND 51-42-21.
- [SDR REXA2017032900438](https://openairdocs.org/sdr/REXA2017032900438.md): Crossbeam · corroded · Mar 29, 2017 · N306PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > LT 280 CROSSBEAM IS CORRODED OUT OF LIMITS. REMOVED AND REPLACED WITH NEW BEAM PER SRM 51-42-06, 51-42-13 AND 51-42-21.
- [SDR REXA2017032800434](https://openairdocs.org/sdr/REXA2017032800434.md): Door Sill · corroded · Mar 28, 2017 · N306PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > RT FLOOR SILL AT FS 280 HAS CORROSION AT THE TOP AND BOTTOM SIDE IN CABIN. OUT OF LIMITS. CUT OUT DAMAGE AND REPAIRED PER SRM 53-21-43.
- [SDR REXA2017032800435](https://openairdocs.org/sdr/REXA2017032800435.md): Diaphragm · corroded · Mar 28, 2017 · N306PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > DIAPHRAM JUST TO THE LEFT OF STGR 27 HAS CORROSION ON BOTH SIDES BETWEEN FRAMES 364 AND 349, IN THE FWD E & E BAY. OUT OF LIMITS. REMOVED AND REPLACED DIAPHRAM LEFT OF STGR 27 FR 364- FR 349 IAW SRM 51-42-06 + 51-42-21.
- [SDR REXA2017032800437](https://openairdocs.org/sdr/REXA2017032800437.md): Floorbeam · corroded · Mar 28, 2017 · N306PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > FWD ANGLE SIDE OF 280 BEAM HAS CORROSION BETWEEN LBL 12 AND RBL 12, IN FLT DECK BELOW FLOOR. REMOVED AND REPLACED WITH NEW FLOOR SUPPORT PER SRM 51-42-06.
- [SDR REXA2016062701158](https://openairdocs.org/sdr/REXA2016062701158.md): Pbe · unserviceable · Jun 27, 2016 · N306PQ · Cndair CL6002D24 · Emergency Equipment
  > COCKPIT PBE VACUUM SEAL BROKEN. INSTALLED SERVICEABLE PBE IAW AMM 35-31-06.
- [SDR REXA2015060600562](https://openairdocs.org/sdr/REXA2015060600562.md): Unknown · odor · Jun 6, 2015 · N306PQ · Cndair CL6002D24 · Air Distribution System
  > WITH APU ON & BOTH PACKS ON ENS OFF, INSTANT SMELL OF SMOLDERING PLASTIC & RUBBER. MOSTLY IN FLIGHT DECK BUT THROUGHOUT ACFT. NO FAULTS FOR ANY ASSOCIATED SYSTEMS NOTED IN MDC. INSPECTED AFT EQUIP BAY, NO DISCREPANCIES NOTED. PERFORMED APU BLEED AIR OPS CH
- [SDR REXA2015032600353](https://openairdocs.org/sdr/REXA2015032600353.md): Escape Hatch · out of adjust · Mar 26, 2015 · N306PQ · Cndair CL6002D24 · Emergency Exits
  > CREW HATCH LEAKING AT RT CORNER LOWER PART OF HATCH. INSPECTED FITS & CLEARANCES OF CREW ESCAPE HATCH AS WELL AS SEAL & HATCH LOCKING PINS & RECEPTACLES FOR SECURITY. FOUND HATCH TO BE OUT OF ADJUSTMENT & RIG LE DOWN MORE THAN.070"". SEAL OKAY IAW MM 52-22
- [SDR REXA2015030300278](https://openairdocs.org/sdr/REXA2015030300278.md): Seal · lack of lube · Mar 3, 2015 · N306PQ · Cndair CL6002D24 · Emergency Exits
  > CREW ESCAPE HATCH LEAKING WATER. LUBRICATED THE CREW ESCAPE HATCH SEAL IAW AMM 12-20-52 PARA 4 STEP A 3.
- [SDR REXA2014122201199](https://openairdocs.org/sdr/REXA2014122201199.md): Light · unsecure · Dec 22, 2014 · N306PQ · Cndair CL6002D24 · Emergency Lighting
  > EMERGENCY FLOOR PATH LIGHTING UNSECURE IN FWD GALLEY, LT SIDE & DIRECTLY BEHIND FWD LAVATORY ON RT SIDE. SECURED EMER FLOOR PATH IAW AMM 33-51-01.
- [SDR REXA2014102001057](https://openairdocs.org/sdr/REXA2014102001057.md): Light · unsecure · Oct 19, 2014 · N306PQ · Cndair CL6002D24 · Emergency Lighting
  > FLOOR STRIP IN FRONT OF GALLEY CART B CAME UP IN FLIGHT. SECURED EMER FLOOR STRIP IAW AMM 33-51-01. NO OTHER DEFECTS NOTED AT THIS TIME.

Next page: https://openairdocs.org/aircraft/N306PQ/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N306PQ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N306PQ/reports

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